Format for CRZ PERF tables

Columns delimited with ;

First column is altitude

Second column is FF per engine in kg/hr

Column contains values for weights ranging from 140t to 290t in 10t increments
Delimited with ,

Third column is IAS

If single value, apply to all weights
If multiple values, apply to respective weights (delimited with ,)

Fourth column is MACH

If single value, apply to all weights
If multiple values, apply to respective weights (delimited with ,)

Format for ECON tables

2d matrix of mach values

Columns delimited with ,
One file per altitude and MMO combination

First index is weight (equates to the lines in the file)

Must be of 140, 150, 160, 170, 180, 190, 200, 210, 220, 230, 240, 250, 260, 270, 280, or 290

Second index is CI (equates to the columns in a line)

Must be in range [0, 999]

Format for raw curve tables

2d matrix of curve parameters

Columns delimited with ;
Parameters delimited with ,, ordered a, b, c

First index is altitude (equates to lines in the file)

Must be of 250, 270, 290, 310, 330, 350, 370, 390, 410, or 430

Second index is weight (equates to the columns in a line)

Must be of 140, 150, 160, 170, 180, 190, 200, 210, 220, 230, 240, 250, 260, 270, 280, or 290

Usage of function


  f(x) = a \cdot \sqrt x + b \cdot x + c

Extract parameters a,b,c from the table
x is the CI and must be in range [0,999]
f(x) is the mach number for the given altitude, weight, CI, and MMO

Conversion of weight to index

f(x) = \frac{x - 140}{10}

x is weight (see range restrictions where applicable)
f(x) is the resulting index for the LUTs

Conversion of altitude to index

f(x) = \frac{x - 250}{20}

x is altitude (see range restrictions where applicable)
f(x) is the resulting index for the LUTs

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